A dual-state propulsion aircraft includes an aircraft fuselage; and at least one dual-state propulsion system, including a fixed nacelle, a rotatable nacelle optionally including a front curved section and rear straight section, mechanical nacelle rotation stops, mechanical shaft rotation stops, a motor, and a thruster with pivotable blades; such that the at least one dual-state propulsion system is rotatable to a first system position configured for horizontal flight and to a second system position configured for vertical flight.
Dual-state rotatable propulsion system
09.11.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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